This report discusses the development of a simulation model of an aircraft landing gear describing its typical non-linear behaviour. The development of the design tool -which correlates the actual design parameters with the performance of the gear- is a part of the research project that investigates the estimation of the nonlinear dynamical system, which an aircraft landing gear is. This project is a joint effort by the Eindhoven University of Technology and DAF Special Products.
The non-linear parts of the simulation model are implemented in the general purpose multi body program DADS, which is based on time integration procedures.
TIRE MODELS IN AIRCRAFT LANDING GEAR SIMULATION
Vehicle System Dynamics ; 21 , sup1 ; 108-115
1992-01-01
8 pages
Aufsatz (Zeitschrift)
Elektronische Ressource
Unbekannt
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